| 摘要 |
PROBLEM TO BE SOLVED: To propose an air-to-ground or air-to-ship missile providing the detonation timing of a nose by computing a relative distance based on the image information and its own flying speed without changing the own heading direction when the size of a target is unknown. SOLUTION: This missile comprises a fuselage and steering wings. The fuselage is provided inside with a camera for obtaining the image of the target; an inertial device for obtaining the own flying speed; the nose for destroying the target; a detonating fuse for detonating the nose; and a control device for extracting the feature points of the image of the camera to detect the number of pixels, computing the relative distance to the target from a change rate of the number of pixels to time, a sampling time and the own flying speed obtained from the inertial device, and transmitting a detonation signal to the detonating fuse when reaching a predetermined detonation distance. COPYRIGHT: (C)2005,JPO&NCIPI
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